The design experience associated with a benchmark aeroelastic design of an out of production transport aircraft is discussed. Current work being performed on a high aspect ratio wing design is reported. The Preliminary Aeroelastic Design of Structures (PADS) system is briefly summarized and some operational aspects of generating the design in an automated aeroelastic design environment are discussed.
Some experiences in aircraft aeroelastic design using Preliminary Aeroelastic Design of Structures (PAD)
1984-01-01
Conference paper
No indication
English
Influence of Aeroelastic Effects on Preliminary Aircraft Design
British Library Conference Proceedings | 2000
|Aeroelastic Problems in aircraft design
TIBKAT | 1979
|